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WO1992016981A1 - Dual band integrated lnb feedhorn system - Google Patents

Dual band integrated lnb feedhorn system Download PDF

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Publication number
WO1992016981A1
WO1992016981A1 PCT/US1991/001966 US9101966W WO9216981A1 WO 1992016981 A1 WO1992016981 A1 WO 1992016981A1 US 9101966 W US9101966 W US 9101966W WO 9216981 A1 WO9216981 A1 WO 9216981A1
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WO
WIPO (PCT)
Prior art keywords
waveguide
band
low noise
energy
modulated
Prior art date
Application number
PCT/US1991/001966
Other languages
French (fr)
Inventor
James Marvin Harris
Original Assignee
Gardiner Communications Corporation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Gardiner Communications Corporation filed Critical Gardiner Communications Corporation
Publication of WO1992016981A1 publication Critical patent/WO1992016981A1/en

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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/22Supports; Mounting means by structural association with other equipment or articles
    • H01Q1/24Supports; Mounting means by structural association with other equipment or articles with receiving set
    • H01Q1/247Supports; Mounting means by structural association with other equipment or articles with receiving set with frequency mixer, e.g. for direct satellite reception or Doppler radar
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q5/00Arrangements for simultaneous operation of antennas on two or more different wavebands, e.g. dual-band or multi-band arrangements
    • H01Q5/40Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements
    • H01Q5/45Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements using two or more feeds in association with a common reflecting, diffracting or refracting device
    • H01Q5/47Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements using two or more feeds in association with a common reflecting, diffracting or refracting device with a coaxial arrangement of the feeds

Definitions

  • Microwave communication systems include one or more satellites receiving signals transmitted to it by an earth station.
  • the satellites amplify and send this information to other earth stations on new carrier frequencies.
  • a frequency difference of about 2 GHz prevents interference between the uplink and downlink transmissions.
  • all geostationary satellites operate in one of the following three bands: Old Band Uplink Downlink Orbit Separation
  • Known earth stations include a parabolic (dish) reflector for collecting the microwave energy transmitted by the satellite.
  • the dish focuses the reflected energy on a feedhom assembly located at a focal point in front of the dish.
  • An entire feedhorn assembly typically includes a feedhorn, a section of waveguide, a polarizer, and a low noise amplifier (LNA) plus associated cable.
  • the LNA circuitry includes a power module for protecting the circuit against power surges or spikes.
  • the power module is typically included in the LNA package which adds, to the bulk and weight of the feedhorn
  • the microwave energy transmitted by satellites typically is polarized vertically and horizontally to double the number of transponders available.
  • a good example of the use of dual polarization on a satellite is the RCA Statcom IIIR which operates at C band (4
  • the twelve odd-numbered transponders utilize the vertically polarized electric field, and the twelve even-numbered transponders utilize the horizontally polarized electric field.
  • Polarizers increase substantially power insertion
  • receiving antenna to correspond to the polarization of the set of transponders generating the desired signals in order to receive those signals.
  • Some earth station antennae have dual polarized feeds which are capable of receiving both polarizations simultaneously and thus can receive any or all of the 24 transponders with no further adjustment of the antenna feed.
  • Such dual systems are very expensive which prohibits their use in the private segment of the commercial market. Nevertheless, even for this application,
  • the antennae should be capable of receiving television programs from all of the satellites and from all of the transponders on each of the satellites.
  • the antenna must be capable of responding to either horizontal polarization or vertical polarization of the frequency bands being used, namely, the C and Ku bands.
  • some satellites may have their polarizations skewed from either the vertical or horizontal positions.
  • the antenna must be positioned to respond to the
  • the motor is controlled by the operator to position the feed assembly such that its polarization coincides to that of the transmitting satellite.
  • the feed assembly was bulky and heavy; thus, rotation of the feed assembly without wobble by the motor
  • a septum is a metal plate positioned across the waveguide.
  • the lines of an electric field are all normal to a plane which passes horizontally through the center of the waveguide. In a circular waveguide the plane is the horizontal diameter.
  • the septum will not block or attenuate the wave nor will it cause reflections to occur so long as it is a relatively thin conducting sheet.
  • the septum can be of any length, and the wave as it travels through the guide will reform after it has passed by the septum into a wave identical to the original wave. In effect the electric field lines being normal to the septum do not see the septum, and the wave is said to be cross polarized with respect to the septum.
  • septum included spaced diametric conducting pins mounted across the diameter of the circular waveguide in the same plane as the previously described septum, and spaced along the longitudinal axis of the guide in relatively close proximity (small fractions of a wavelength) one to another. Each pin was slightly rotated a few degrees (only enough to prevent discontinuities) and a gradual rotation of the polarization began without upsetting the wave propagation in the waveguide. If the pins themselves are rotated as described in U.S. Patent Nos. 3,287,729 and 3,296,558, the entire feed assembly need not be rotated.
  • the filament comprises a series of interconnected legs for transverse orientation to wave propagation at the diameter of a circular waveguide. Each leg is approximately equal in length but slightly less than the diameter of the waveguide.
  • the filament te ⁇ ninates in a leg at each end. One end leg is rigidly mounted to the wall of the desired waveguide input to the LNA and the other end is securely fastened to a rotatable sleeve for rotation around the longitudinal axis of the waveguide.
  • the only driven element is the leg nearest the aperture of the feed.
  • the serpentine shape of the filament assures accurate leg-to-leg spacing and successively small progression of leg-to-leg rotation. By appropriate selection of a resilient material, rotation of the legs of the filament is repeatable. More information about the serpentine
  • the disadvantage of the above-described feed assembly structures include their rotational-prohibitive size and weight, the substantial power insertion loss attending the use of septums as polarizering elements, heat destruction of the low noise amplifier (LNA) or low noise “block” (LNB) or module resulting from including the power regulator within the LNA or LNB where heat generated by regulating high voltages or transients destroys not only the power regulator but also the LNA or LNB; and decreased aiming accuracy attending the narrow half power beamwidth produced by these systems.
  • LNA low noise amplifier
  • LNB low noise "block”
  • a LNB is a LNA combined with a frequency downconverter and IF amplifier for producing modulated IF signals.
  • LNB dual band integrated low noise block
  • Another object of the invention is to provide a dual band integrated LNB feedhom system having substantially reduced power insertion loss.
  • Yet another object of the invention is to provide a dual band integrated LNB feedhom system configured to reduce substantially heat damage resulting from power surges and to reduce maintenance time and cost.
  • Still another object of the invention is to provide a dual band integrated LNB feedhom system having at one band an increased half power beamwidth thereby reducing the aiming accuracy requirement for the antenna.
  • a further object of the invention is to provide a dual band integrated LNB feedhom system having increased performance.
  • the dual band integrated LNB feedhom system in accordance with the subject matter of the invention comprises a feedhom assembly having a rotatable subassembly including first and second concentrically formed waveguides and first and second low noise blocks (LNB's) connected to power extraction probes mounted in waveguides.
  • the power extraction probes when the subassembly is rotated, provide polarization corresponding to the polarization of a transmitter with substantially reduced power insertion loss.
  • the reduced insertion loss enables defocusing of the Ku band waveguide to widen the half power beamwidth of the incoming modulated carrier signals to improve aiming accuracy without decreasing the gain and degrading performance.
  • the C band waveguide has an adjustable scalar for focusing at the focal point of the antenna dish.
  • Power modules are provided outside the LNAs or LNBs for transferring heat directly to the atmosphere and for ready replacement when destroyed by power surges.
  • FIGURE 1 is a block diagram of the dual band integrated LNB feedhom system in accordance with the subject matter of the invention.
  • FIGURE 2 is a sectional view of the dual band integrated LNB feedhom system in accordance with the subject matter of the invention.
  • the earth station 10 of a communication satellite system includes a parabolic
  • a dual band feedhom 16 is mounted at the focal point of the dish for receiving the reflected energy for two block downconverters (BDCs) 18-one for each band.
  • Each block downconverter is, for example, a Gardiner Communications Corporation 200-9545-001 device.
  • the device includes a three-stage low noise amplifier 20 for amplifying the incoming signals to a working level, a mixer 22 connected to a local r-f oscillator 24 for combining the incoming modulated r-f signal with the signal of the local r-f oscillator to produce a modulated i-f signal, and a two stage intermediate frequency (IF) amplifier 26 for amplifying the IF signals to a working level.
  • IF intermediate frequency
  • a pair of power modules 28 are connected to the outputs of the block downconverters 18.
  • Each power module includes a transient suppressor and a + 15 volt regulator connected by a coaxial cable 30 to a receiver (demodulator) 32.
  • the power modules pass the modulated IF signals to the receiver (demodulator) and receive dc power through the inner conductor of the coaxial cables 30 for the block downconverter.
  • the receiver (demodulator) may be at any distance from the power module, the dc voltage may be for a maximum distance between the demodulator and power module (about 500 ft.); thus, the power modules regulate the dc power received and suppress any transient voltage received to protect the block downconverter from destructive voltages and heat generated by power modules.
  • the receiver (demodulator) 32 is selectively connected to one of the two bands for outputting TV channel 3 or 4 signals to a television set 34, for example, for processing.
  • a suitable receiver (demodulator) is a Satellite Technology Services receiver model SR 100. Referring now to FIGURE 2, a preferred embodiment of the dual band integrated
  • a cylindrical housing 36 which is connected to LNB feedhom system of the present invention is shown.
  • a cylindrical housing 36 which is connected to LNB feedhom system of the present invention.
  • the first end 38 supports an inverted U-shaped support 44 by screws 42.
  • the cross-arm has
  • servomotor mounts 46 extending upwardly towards the first end 38 and walls forming a centrally disposed aperture between the motor mounts.
  • a servomotor 48 is attached to the motor mounts with its drive shaft 50 extending downwardly through the aperture.
  • a power cable takeup spool 52 is attached to a lower portion of the drive shaft.
  • Coaxial cables 54 and 56 have first portions attached to a cable retainer 62 by corresponding fastener screws.
  • the cable retainer 62 is attached to the cross bar of the U-shaped member 44. The ends of the first portions of the cables 54 and 56 are attached to a pair
  • the drive shaft 50 has its end opposite the motor attachment end fastened to a horizontally disposed arm of support member 66.
  • Support member 66 is rotated by any rotation of the drive shaft.
  • a cable retainer 67 is attached to the horizontally disposed arm of support member 66 and the cables 54 and 56 have second portions fastened to the cable retainer.
  • a vertically disposed leg of support member 66 supports a cable connector 68 for connecting coaxial cable 54 to a C band low noise block downconverter (FIGS. 1 and 2) 18 for receiving the modulated IF signal output.
  • the input to the C band LNB 18 is connected to a probe 70 of a C band coaxial cable waveguide 72 forming a portion of feedhom 16.
  • the C band waveguide has a first end attached to the leg of support member 66, a body portion extending downwardly into a cylindrically cup-shaped member 74 attached to aperture forming walls of end 40 of housing 36, and a second end having a pivot 76 mounted in the bottom of the cup-shaped member for rotation support.
  • the end of the C band coaxial waveguide is to be positioned at the focal point of the dish 12.
  • a Ku band waveguide 78 forms the remainder of the feedhom 16.
  • the Ku band is slidable mounted in the inner conductor 80 of the C band coaxial waveguide 72 for proper defocusing.
  • a clamp 81 secures the Ku band waveguide in its proper position.
  • a probe 82 connects the output of the Ku band waveguide to a Ku band low noise amplifier 20, which in turn is connected to a Ku band block downconverter 18' including the mixer 22, local oscillator 24, and IF amplifier 26 (see FIG. 1) which together with the LNA forms the block downconverter 18.
  • the output of Ku band block downconverter 18 is connected through coaxial cable connector 83 to coaxial cable 56.
  • a scalar 84 is adjustably connected to the cylindrically cup-shaped member 74.
  • the scalar prevents energy approaching the feedhom as noise from the rear from entering the feedhom.
  • the dual band integrated LNB feedhom system is equipped for independent C band and Ku band focusing.
  • the feedhom system is attached with the end of the C band waveguide at the focal point of the parabolic reflector 12, and the Ku band waveguide is defocused in an amount to allow for wider half-power beamwidth without significantly affecting the gain of the Ku band feed system.
  • the result is that neither the C band nor the Ku band performance is sacrificed.
  • the aiming accuracy of the Ku band is improved by defocusing to increase the half power beamwidth.
  • servomotor 48 is actuated by a remotely positioned controller to rotate the C band and Ku band waveguides to align their energy output probes with the polarization of the incoming modulated RF energy.
  • the output probes combine their normal output function with the polarizer function of polarizers to obtain a power savings sufficient to provide a wider than normal half power beamwidth. This result increases the aiming accuracy and compensates for the defocusing of the Ku band without significantly affecting its gain.

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  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Waveguide Aerials (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

A dual band integrated feedhorn (16) includes a housing (36) having a rotatable support (66) for a C band coaxial waveguide (72), a clamp (81) for a Ku band waveguide (78), a Ku band waveguide (78) slidably mounted in the clamp (81) for focus adjustment, and a pair of low noise blocks (18) connected to the waveguide output probes (70, 82) for downconverting their incoming modulated carrier C and Ku band signals to modulated IF signals. A servo (48) drives the support member to position the waveguide's energy output coupling probes (70, 82) to match the polarization of the incoming RF energy; thus, eliminating the need for polarizers and reducing insertion loss significantly. The reduced insertion loss enables defocusing of the Ku band waveguide (78) to widen the half power beamwidth to improve aiming accuracy without decreasing the gain and degrading performance. A position adjustable scalar (84) and a pair of power modules (28) are attached exteriorly of the housing. The scalar (84) is positioned adjacent the end of the C band waveguide (72) for focusing the C band waveguide (72). The power modules (28) include transient suppressors and voltage regulators connected to the pair of low noise blocks (18) for suppressing incoming transients and regulating the incoming dc voltage while outputting the modulated IF carrier signals. Thus, heat generated by the power modules (28) is kept from the low noise blocks (18), resulting in improved operating performance and increased life.

Description

DUAL BAND INTEGRATED LNB FEEDHORN SYSTEM This invention relates to communication microwave devices and more particularly to a dual band integrated low noise block (LNB) feedhorn system. BACKGROUND OF THE INVENTION
Microwave communication systems include one or more satellites receiving signals transmitted to it by an earth station. The satellites amplify and send this information to other earth stations on new carrier frequencies. A frequency difference of about 2 GHz prevents interference between the uplink and downlink transmissions. For example, all geostationary satellites operate in one of the following three bands: Old Band Uplink Downlink Orbit Separation
Figure imgf000003_0001
In certain earth locations such as the United States the communication systems operate at C band; while, in Europe the communication systems operate at Ku band. It is becoming increasingly desirable for earth stations to receive the programs of both the C band and the Ku band.
Known earth stations include a parabolic (dish) reflector for collecting the microwave energy transmitted by the satellite. The dish focuses the reflected energy on a feedhom assembly located at a focal point in front of the dish. An entire feedhorn assembly typically includes a feedhorn, a section of waveguide, a polarizer, and a low noise amplifier (LNA) plus associated cable. The LNA circuitry includes a power module for protecting the circuit against power surges or spikes. The power module is typically included in the LNA package which adds, to the bulk and weight of the feedhorn
assembly as well as to the heat generated in the LNA package. The heat dissipated during a power surge can destroy the LNA which it was designed to protect.
The microwave energy transmitted by satellites typically is polarized vertically and horizontally to double the number of transponders available. A good example of the use of dual polarization on a satellite is the RCA Statcom IIIR which operates at C band (4
GHz) with 24 transponders. The twelve odd-numbered transponders utilize the vertically polarized electric field, and the twelve even-numbered transponders utilize the horizontally polarized electric field. Polarizers increase substantially power insertion
losses.
At an earth station receiving site it is necessary to adjust the polarization of the
receiving antenna to correspond to the polarization of the set of transponders generating the desired signals in order to receive those signals. Some earth station antennae have dual polarized feeds which are capable of receiving both polarizations simultaneously and thus can receive any or all of the 24 transponders with no further adjustment of the antenna feed. Such dual systems, however, are very expensive which prohibits their use in the private segment of the commercial market. Nevertheless, even for this application,
the antennae should be capable of receiving television programs from all of the satellites and from all of the transponders on each of the satellites. Thus, for best results (pictures) the antenna must be capable of responding to either horizontal polarization or vertical polarization of the frequency bands being used, namely, the C and Ku bands.
Also, some satellites may have their polarizations skewed from either the vertical or horizontal positions. In this case the antenna must be positioned to respond to the
signals having skewed polarizations.
Early earth station designs utilized a motor to rotate the entire feed assembly.
The motor is controlled by the operator to position the feed assembly such that its polarization coincides to that of the transmitting satellite. However, the feed assembly was bulky and heavy; thus, rotation of the feed assembly without wobble by the motor
drive was difficult. Any wobble of the feedhorn during rotation caused the antenna beam to depart from true boresight along the focal axis, and the signal from the satellite was not in the maximum of the receiving antenna pattern. To alleviate the wobble problem,
efforts were directed toward obtaining the desired polarization using a stationary feed assembly. In addition, wind forces result in decreased aiming accuracy and a loss of the incoming signals.
These efforts included the use of a septum in the rotating waveguide. A septum is a metal plate positioned across the waveguide. The lines of an electric field are all normal to a plane which passes horizontally through the center of the waveguide. In a circular waveguide the plane is the horizontal diameter. When properly aligned, the septum will not block or attenuate the wave nor will it cause reflections to occur so long as it is a relatively thin conducting sheet. The septum can be of any length, and the wave as it travels through the guide will reform after it has passed by the septum into a wave identical to the original wave. In effect the electric field lines being normal to the septum do not see the septum, and the wave is said to be cross polarized with respect to the septum.
Another form of the septum included spaced diametric conducting pins mounted across the diameter of the circular waveguide in the same plane as the previously described septum, and spaced along the longitudinal axis of the guide in relatively close proximity (small fractions of a wavelength) one to another. Each pin was slightly rotated a few degrees (only enough to prevent discontinuities) and a gradual rotation of the polarization began without upsetting the wave propagation in the waveguide. If the pins themselves are rotated as described in U.S. Patent Nos. 3,287,729 and 3,296,558, the entire feed assembly need not be rotated.
To avoid the need for a complex pin rotational mechanism, a twistable serpentine- shaped filament was developed. The filament comprises a series of interconnected legs for transverse orientation to wave propagation at the diameter of a circular waveguide. Each leg is approximately equal in length but slightly less than the diameter of the waveguide. The filament teπninates in a leg at each end. One end leg is rigidly mounted to the wall of the desired waveguide input to the LNA and the other end is securely fastened to a rotatable sleeve for rotation around the longitudinal axis of the waveguide. Thus, the only driven element is the leg nearest the aperture of the feed. The serpentine shape of the filament assures accurate leg-to-leg spacing and successively small progression of leg-to-leg rotation. By appropriate selection of a resilient material, rotation of the legs of the filament is repeatable. More information about the serpentine
filament is given in U.S. Patent No. 4,503,379.
The disadvantage of the above-described feed assembly structures include their rotational-prohibitive size and weight, the substantial power insertion loss attending the use of septums as polarizering elements, heat destruction of the low noise amplifier (LNA) or low noise "block" (LNB) or module resulting from including the power regulator within the LNA or LNB where heat generated by regulating high voltages or transients destroys not only the power regulator but also the LNA or LNB; and decreased aiming accuracy attending the narrow half power beamwidth produced by these systems. A LNB is a LNA combined with a frequency downconverter and IF amplifier for producing modulated IF signals.
SUMMARY OF THE INVENTION
Accordingly it is an object of the present invention to provide a dual band integrated low noise block (LNB) feedhom system of a weight and size suitable for use as an earth station feed assembly receiving with substantially reduced wobble power generated at two different frequency bands by a communication satellite.
Another object of the invention is to provide a dual band integrated LNB feedhom system having substantially reduced power insertion loss.
Yet another object of the invention is to provide a dual band integrated LNB feedhom system configured to reduce substantially heat damage resulting from power surges and to reduce maintenance time and cost.
Still another object of the invention is to provide a dual band integrated LNB feedhom system having at one band an increased half power beamwidth thereby reducing the aiming accuracy requirement for the antenna.
A further object of the invention is to provide a dual band integrated LNB feedhom system having increased performance.
Briefly stated the dual band integrated LNB feedhom system in accordance with the subject matter of the invention comprises a feedhom assembly having a rotatable subassembly including first and second concentrically formed waveguides and first and second low noise blocks (LNB's) connected to power extraction probes mounted in waveguides. The power extraction probes, when the subassembly is rotated, provide polarization corresponding to the polarization of a transmitter with substantially reduced power insertion loss.
The reduced insertion loss enables defocusing of the Ku band waveguide to widen the half power beamwidth of the incoming modulated carrier signals to improve aiming accuracy without decreasing the gain and degrading performance. The C band waveguide has an adjustable scalar for focusing at the focal point of the antenna dish.
Power modules are provided outside the LNAs or LNBs for transferring heat directly to the atmosphere and for ready replacement when destroyed by power surges. BRIEF DESCRIPΗON OF THE DRAWINGS
Other objects and features of the invention will become more readily apparent from the following detailed description when read in conjunction with the accompanying drawings in which:
FIGURE 1 is a block diagram of the dual band integrated LNB feedhom system in accordance with the subject matter of the invention.
FIGURE 2 is a sectional view of the dual band integrated LNB feedhom system in accordance with the subject matter of the invention.
DETAILED DESCRIPΗON OF THE PREFERRED EMBODIMENT
Referring now to Figures 1 and 2, a description of the preferred embodiment of the present invention is given.
The earth station 10 of a communication satellite system includes a parabolic
reflector (dish) 12 mounted upon a support 14 for illumination by a communications satellite transmitting modulated r-f signals at, for example, C band and Ku band frequencies. A dual band feedhom 16 is mounted at the focal point of the dish for receiving the reflected energy for two block downconverters (BDCs) 18-one for each band.
Each block downconverter is, for example, a Gardiner Communications Corporation 200-9545-001 device. The device includes a three-stage low noise amplifier 20 for amplifying the incoming signals to a working level, a mixer 22 connected to a local r-f oscillator 24 for combining the incoming modulated r-f signal with the signal of the local r-f oscillator to produce a modulated i-f signal, and a two stage intermediate frequency (IF) amplifier 26 for amplifying the IF signals to a working level.
A pair of power modules 28 are connected to the outputs of the block downconverters 18. Each power module includes a transient suppressor and a + 15 volt regulator connected by a coaxial cable 30 to a receiver (demodulator) 32. The power modules pass the modulated IF signals to the receiver (demodulator) and receive dc power through the inner conductor of the coaxial cables 30 for the block downconverter. As the receiver (demodulator) may be at any distance from the power module, the dc voltage may be for a maximum distance between the demodulator and power module (about 500 ft.); thus, the power modules regulate the dc power received and suppress any transient voltage received to protect the block downconverter from destructive voltages and heat generated by power modules.
The receiver (demodulator) 32 is selectively connected to one of the two bands for outputting TV channel 3 or 4 signals to a television set 34, for example, for processing. A suitable receiver (demodulator) is a Satellite Technology Services receiver model SR 100. Referring now to FIGURE 2, a preferred embodiment of the dual band integrated
LNB feedhom system of the present invention is shown. A cylindrical housing 36 which
may be of aluminum or plastic has first and second opposing ends 38 and 40. The first end 38 supports an inverted U-shaped support 44 by screws 42. The cross-arm has
servomotor mounts 46 extending upwardly towards the first end 38 and walls forming a centrally disposed aperture between the motor mounts. A servomotor 48 is attached to the motor mounts with its drive shaft 50 extending downwardly through the aperture. A power cable takeup spool 52 is attached to a lower portion of the drive shaft. IF power connecting cables 54 and 56 are wound upon the spool in grooves 58 and 60. Coaxial cables 54 and 56 have first portions attached to a cable retainer 62 by corresponding fastener screws. The cable retainer 62 is attached to the cross bar of the U-shaped member 44. The ends of the first portions of the cables 54 and 56 are attached to a pair
of coaxial cable connectors 64 attached to apertures forming walls of the second end 40 of housing 36. Only one of the connectors 64 is shown in FIGURE 2. The pair of power
modules 28, of which only one is shown, are connected to the pair of power connectors
64 exteriorly of the housing 36.
The drive shaft 50 has its end opposite the motor attachment end fastened to a horizontally disposed arm of support member 66. Support member 66 is rotated by any rotation of the drive shaft. A cable retainer 67 is attached to the horizontally disposed arm of support member 66 and the cables 54 and 56 have second portions fastened to the cable retainer. A vertically disposed leg of support member 66 supports a cable connector 68 for connecting coaxial cable 54 to a C band low noise block downconverter (FIGS. 1 and 2) 18 for receiving the modulated IF signal output.
The input to the C band LNB 18 is connected to a probe 70 of a C band coaxial cable waveguide 72 forming a portion of feedhom 16. The C band waveguide has a first end attached to the leg of support member 66, a body portion extending downwardly into a cylindrically cup-shaped member 74 attached to aperture forming walls of end 40 of housing 36, and a second end having a pivot 76 mounted in the bottom of the cup-shaped member for rotation support. The end of the C band coaxial waveguide is to be positioned at the focal point of the dish 12.
A Ku band waveguide 78 forms the remainder of the feedhom 16. The Ku band is slidable mounted in the inner conductor 80 of the C band coaxial waveguide 72 for proper defocusing. A clamp 81 secures the Ku band waveguide in its proper position. A probe 82 connects the output of the Ku band waveguide to a Ku band low noise amplifier 20, which in turn is connected to a Ku band block downconverter 18' including the mixer 22, local oscillator 24, and IF amplifier 26 (see FIG. 1) which together with the LNA forms the block downconverter 18. The output of Ku band block downconverter 18 is connected through coaxial cable connector 83 to coaxial cable 56.
Finally, a scalar 84 is adjustably connected to the cylindrically cup-shaped member 74. The scalar prevents energy approaching the feedhom as noise from the rear from entering the feedhom.
In operation, the insertion loss is significantly reduced by eliminating polari-ring elements. The dual band integrated LNB feedhom system is equipped for independent C band and Ku band focusing. The feedhom system is attached with the end of the C band waveguide at the focal point of the parabolic reflector 12, and the Ku band waveguide is defocused in an amount to allow for wider half-power beamwidth without significantly affecting the gain of the Ku band feed system. The result is that neither the C band nor the Ku band performance is sacrificed. In addition, the aiming accuracy of the Ku band is improved by defocusing to increase the half power beamwidth.
With the C band waveguide focused and the Ku band properly defocused, the
servomotor 48 is actuated by a remotely positioned controller to rotate the C band and Ku band waveguides to align their energy output probes with the polarization of the incoming modulated RF energy. Thus, the output probes combine their normal output function with the polarizer function of polarizers to obtain a power savings sufficient to provide a wider than normal half power beamwidth. This result increases the aiming accuracy and compensates for the defocusing of the Ku band without significantly affecting its gain.
Although only a single embodiment of this invention has been described, it will be apparent to a person skilled in the art that various modifications to the details of construction shown and described may be made without departing from the scope of this invention.
What is claimed is:

Claims

1. A multi-band integrated LNB feedhom system comprising: a housing having a body portion and first and second ends, a first support means attached to the housing adjacent to the first end for forming a drive motor portion of the housing, a servomotor mounted on the first support means, a second support means contained in
the body portion of the housing and connected to the servomotor for rotation, a plurality of power modules exteriorly attached to the housing, a plurality of low noise block means attached to the second support means for rotation therewith and electrically connected to the plurality of power modules, a cup-shaped member attached to the second end of
the housing for forming with a portion of the housing a compartment for a plurality of waveguide means including a plurality of energy output coupling means electrically connected to the plurality of low noise block means, and first and second waveguide means attached to the second support means for rotation therewith, a focusing means, the first waveguide means connected to the focusing means for focusing modulated RF signals at a first band received from an antenna, a defocusing means, the second waveguide means connected to the defocusing means for defocusing modulated RF signals at a second band received from the antenna,
whereby with the band of the first waveguide means being focused and the band of the second waveguide means being defocused and the second support means rotated by the servomotor to align the first and second waveguide means and plurality of low noise block means with the polarization of incoming modulated RF energy, the first and second waveguide means and plurality of low noise block means combine to perform the polarizer function thereby alleviating the need for additional polarizing elements and their power loss to provide a power savings sufficient for a wider than typical half power
beamwidth for increasing the aiming accuracy while compensating for the defocusing of the band of the second waveguide means without substantially affecting its gain.
2. A multi-band integrated LNB feedhom system according to Claim 1 further including a corresponding plurality of coaxial cables interconnecting the plurality of low noise block means to the plurality of power modules and a coaxial cable spool connected to the servo drive shaft for selectively storing coaxial cable portions excessive to the rotation requirements.
3. A LNB feedhom system comprising: a first and second support means, means mounted on the first support means and connected to the second support means for rotatmg the second support means, at least one low noise block means and at least one waveguide means electrically connected for processing modulated RF energy having a preselected polarization, said at least one waveguide means including a waveguide and a probe mounted in the waveguide for connecting modulated RF energy in the waveguide to the at least one low noise block means, said at least one low noise block means and waveguide of the at least one waveguide means being connected to the second support means whereby when the second support means is rotated the at least one low noise block means and the waveguide of the at least one waveguide means is rotated for positioning the probe of the at least one waveguide means with respect to the polarization of the modulated RF energy.
4. A LNB feedhom system according to Claim 3 further comprising a housing having an exterior surface and at least one power module attached to the exterior surface of the housing, said power module including a transient voltage suppressor and a voltage regulator electrically connected to the low noise block means and adapted for connection to a remotely positioned receiver or transmitter or both for protecting the low noise
block means from any transient voltage received and heat generated by the voltage regulator, respectively.
5. A method, for operating a multi-band integrated LNB feedhom system having first and second support means, means mounted on the first support means for rotating the second support means, a plurality of low noise block means, a plurality of waveguide means including a plurality of energy probe means electrically connected to the plurality of low noise block means for processing modulated RF energy and a plurality of waveguides connected to the plurality of energy probe means, said plurality of waveguides and plurality of low noise block means connected to the second support means for rotation therewith for polarization positioning of the plurality of energy probe means thereby elj_Lτjinating additional polarizing elements in the energy probe means for polarization section and the loss of energy attending their use, and a plurality of focusing means connected to the plurality of waveguides for focusing the modulated RF energy, consisting of defocusing a selected one of the plurality of waveguides for defocusing a selected band of modulated RF energy to provide a wider than typical half power beamwidth for increasing aiming accuracy without substantially affecting its gain.
PCT/US1991/001966 1988-12-01 1991-03-25 Dual band integrated lnb feedhorn system WO1992016981A1 (en)

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US07/278,589 US5005023A (en) 1988-12-01 1988-12-01 Dual band integrated LNB feedhorn system

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5963109A (en) * 1995-02-21 1999-10-05 U.S. Philips Corporation Converter for a satellite antenna having a replaceable core module

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3260781B2 (en) * 1990-09-06 2002-02-25 ルーセント テクノロジーズ インコーポレイテッド Antenna assembly
EP0523770B1 (en) * 1991-07-15 1999-09-29 Matsushita Electric Works, Ltd. Low-noise-block downconverter for use with flat antenna receiving dual polarized electromagnetic waves
DE69308906T2 (en) * 1992-01-21 1997-09-11 Sharp Kk Waveguide coaxial transition and converter for satellite broadcast antenna with such a waveguide
CA2130750A1 (en) * 1992-02-24 1993-09-02 John Weber Dual band signal receiver
US6366244B1 (en) * 1993-03-11 2002-04-02 Southern California Edison Company Planar dual band microstrip or slotted waveguide array antenna for all weather applications
EP0683561A1 (en) * 1994-05-18 1995-11-22 Guan-Wu Wang Low-cost low noise block down-converter with a self-oscillating mixer for satellite broadcast receivers
JP3071136B2 (en) * 1995-03-07 2000-07-31 シャープ株式会社 Terminal structure and universal LNB using this
US5793334A (en) * 1996-08-14 1998-08-11 L-3 Communications Corporation Shrouded horn feed assembly
US5818396A (en) * 1996-08-14 1998-10-06 L-3 Communications Corporation Launcher for plural band feed system
US5793335A (en) * 1996-08-14 1998-08-11 L-3 Communications Corporation Plural band feed system
US6121939A (en) 1996-11-15 2000-09-19 Yagi Antenna Co., Ltd. Multibeam antenna
US5940737A (en) * 1997-02-27 1999-08-17 Hughes Electronics Corporation Signal selector
GB9900411D0 (en) 1999-01-08 1999-02-24 Cambridge Ind Ltd Multi-frequency antenna feed
US20080211730A1 (en) 2007-01-26 2008-09-04 Woosnam Calvin H Gimbaled Mount System for Satellites
CN102510266B (en) * 2011-12-29 2014-11-19 北京遥测技术研究所 Ku frequency band low-noise amplifier
SE541878C2 (en) * 2018-04-23 2020-01-02 Requtech Ab Multi-band antenna feed arrangement

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4642479A (en) * 1985-04-04 1987-02-10 Motorola, Inc. Power distribution device
US4740795A (en) * 1986-05-28 1988-04-26 Seavey Engineering Associates, Inc. Dual frequency antenna feeding with coincident phase centers
US4821046A (en) * 1986-08-21 1989-04-11 Wilkes Brian J Dual band feed system
US4862187A (en) * 1988-10-24 1989-08-29 Microwave Components And Systems, Inc. Dual band feedhorn with two different dipole sets
US4903037A (en) * 1987-10-02 1990-02-20 Antenna Downlink, Inc. Dual frequency microwave feed assembly

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4538175A (en) * 1980-07-11 1985-08-27 Microdyne Corporation Receive only earth satellite ground station
AT373734B (en) * 1982-02-25 1984-02-10 Feller Josef Gmbh DEVICE FOR SHIELDING DEVICES FROM HIGH-FREQUENCY INTERFERENCE
US4785306A (en) * 1986-01-17 1988-11-15 General Instrument Corporation Dual frequency feed satellite antenna horn
US4819005A (en) * 1986-08-21 1989-04-04 Wilkes Brian J Concentric waveguides for a dual-band feed system
CA1260609A (en) * 1986-09-12 1989-09-26 Her Majesty The Queen, In Right Of Canada, As Represented By The Minister Of National Defence Wide bandwidth multiband feed system with polarization diversity
US4801945A (en) * 1987-07-07 1989-01-31 Janeil Corporation Low loss dual band satellite antenna feed
US4841261A (en) * 1987-09-01 1989-06-20 Augustin Eugene P Microwave rotary junction with external rotary energy coupling

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4642479A (en) * 1985-04-04 1987-02-10 Motorola, Inc. Power distribution device
US4740795A (en) * 1986-05-28 1988-04-26 Seavey Engineering Associates, Inc. Dual frequency antenna feeding with coincident phase centers
US4821046A (en) * 1986-08-21 1989-04-11 Wilkes Brian J Dual band feed system
US4903037A (en) * 1987-10-02 1990-02-20 Antenna Downlink, Inc. Dual frequency microwave feed assembly
US4862187A (en) * 1988-10-24 1989-08-29 Microwave Components And Systems, Inc. Dual band feedhorn with two different dipole sets

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5963109A (en) * 1995-02-21 1999-10-05 U.S. Philips Corporation Converter for a satellite antenna having a replaceable core module

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